Harbin SH-5

The Harbin SH-5 "(Shuishang Hongzhaji), literally "seaborne bomber") is a Chinese maritime patrol amphibious aircraft intended for a wide range of duties, including aerial firefighting, anti-submarine warfare (ASW) and air-sea rescue (SAR). They are used for maritime and search and rescue operations. Only 6 units have been built not counting the prototype; all are in active service except one crashed on May 30, 2013. One is outfitted as a firefighting plane.

Harbin SH-5
Class Aircraft
Type Utility
Manufacturer Harbin Aircraft Industry Group
Production Period 1984 - 1985
Origin China
Country Name Origin Year
China 1976
Country Name Operational Year Retirement Year
China 1986 View
ManufacturerName Production From Production To Quantity
Harbin Aircraft Industry Group 1984 1985 7 View

Research to build a seaplane capable of replacing Beriev Be-6s in service was initiated by the PLANAF in 1968, with designers overhauled from "Objective 3/17", a supersonic canard-wing fighter project. The first prototype flew in 1976; further units were delivered between 1986 and 1990.

Variants

  • SH-5
  • SH-5A Maritime patrol aircraft
  • SH-5B Firefighter

    


Role Maritime patrol amphibian/air-sea rescue
Manufacturer Harbin Aircraft Factory
First flight 3 April 1976
Introduction 1986
Primary user People's Liberation Army Naval Air Force
Produced 1984-1985
Number built


General characteristics

  • Crew: 8
  • Capacity: 10,000 kg (22,000 lb) maximum payload (cargo), 6,000 kg (13,000 lb) maximum weapons load
  • Length: 38.9 m (127 ft 7 in)
  • Wingspan: 36 m (118 ft 1 in)
  • Height: 9.79 m (32 ft 1 in)
  • Wing area: 144 m2 (1,550 sq ft)
  • Empty weight: 25,000 kg (55,116 lb) SAR (Search And Rescue) and Transport
  • 26,500 kg (58,400 lb) ASW (Anti-Submarine Warfare)
  • Gross weight: 36,000 kg (79,366 lb)
  • Max takeoff weight: 45,000 kg (99,208 lb)
  • Fuel capacity: 16,500 kg (36,400 lb) max
  • Powerplant: 4 × Dongan WJ5A turboprop engines, 2,350 kW (3,150 hp) each
  • Propellers: 4-bladed constant speed reversible propellers, 3.8 m (12 ft 6 in) diameter

Performance

  • Maximum speed: 556 km/h; 345 mph (300 kn)
  • Cruise speed: 450 km/h; 280 mph (243 kn) maximum
  • Min Patrol speed: 230 km/h (120 kn; 140 mph)
  • Take-off speed (water): 160 km/h (86 kn; 99 mph)
  • Landing speed (water): 92 km/h (50 kn; 57 mph)
  • Range: 4,756 km; 2,955 mi (2,568 nmi) with maximum fuel
  • Endurance: 15 hours on two engines
  • Service ceiling: 10,250 m (33,629 ft) service ceiling
  • Rate of climb: 9 m/s (1,800 ft/min)
  • Wing loading: 250 kg/m2 (51 lb/sq ft) at 36,000 kg (79,000 lb)
  • 312.5 kg/m² (64 lb/sqft) at 45,000 kg (99,000 lb)
  • Power/mass: 0.302 kW/kg (0.184 hp/lb) at 36,000 kg (79,000 lb)
  • 0.242 kW/kg (0.147 hp/lb) at 45,000 kg (99,000 lb)
  • Take-off run (water): 548 m (1,798 ft)
  • Landing run (water): 240 m (790 ft)

Armament

  • four hardpoints; 6,000 kg (13,000 lb) warload; C-101 ASMs, ASW torpedoes, depth charges; mines; bombs

Avionics

  • Doppler search radar in nose radome; MAD (Magnetic Anomaly Detector) boom extending from the tail of the fuselage

End notes